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Meysam Mahooti


University of Tehran

Con actividad desde 2016

Followers: 17   Following: 0

Mensaje

Programming Languages:
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics

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Enviada


Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications

3 días hace | 58 descargas |

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Positions of solar system bodies
The heliocentric and geocentric positions of the solar system's eight planets, in addition to the Moon and the Sun

4 días hace | 10 descargas |

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Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model

8 días hace | 25 descargas |

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High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)

8 días hace | 69 descargas |

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Satellite Orbit Modeling
Precise modeling of satellite's perturbed motion (special perturbations approach)

9 días hace | 42 descargas |

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Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data

10 días hace | 21 descargas |

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Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements

11 días hace | 24 descargas |

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NASA JPL Development Ephemerides (DE430)
DE430 spans from 1549-12-21 to 2650-01-25 and is based on the International Celestial Reference Frame (version 2.0).

25 días hace | 21 descargas |

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Runge-Kutta-Fehlberg (RKF78)
Fehlberg's 7th and 8th Order Embedded Method

27 días hace | 22 descargas |

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NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.

27 días hace | 48 descargas |

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SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites

4 meses hace | 13 descargas |

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Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets

4 meses hace | 3 descargas |

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Moon Position
Position of the Moon referred to the mean equator and equinox of J2000

4 meses hace | 5 descargas |

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ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa

4 meses hace | 22 descargas |

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Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF

4 meses hace | 11 descargas |

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Radau IIA
Variable-order Radau IIA integrator with step-size control

6 meses hace | 9 descargas |

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Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future

8 meses hace | 11 descargas |

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NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.

8 meses hace | 11 descargas |

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Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)

9 meses hace | 6 descargas |

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Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method

10 meses hace | 16 descargas |

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Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method

10 meses hace | 6 descargas |

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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides

10 meses hace | 8 descargas |

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NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides

12 meses hace | 7 descargas |

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Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.

alrededor de 1 año hace | 18 descargas |

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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times

alrededor de 1 año hace | 4 descargas |

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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times

alrededor de 1 año hace | 5 descargas |

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Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter

más de 1 año hace | 17 descargas |

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Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.

más de 1 año hace | 4 descargas |

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Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.

más de 1 año hace | 16 descargas |

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SGP4/SDP4
SGP4 and SDP4 orbit propagators

más de 1 año hace | 15 descargas |

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